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Park Aerospace F-502 3K 8HS PAN

Park’s F-502 is a MIL-R-9299 phenolic resin system suitable for impregnation on any MIL-C-9084 fabric with a compatible finish. F-502 is used in the manufacture of ablative reinforcements in rocket nozzles, as well as ducting and secondary structures.

Polymer Name: Phenolic Compound

Functions: Prepreg

Reinforcement Material: Carbon Fibers, Glass Fibers

Processing Methods: Compression Molding, Prepreg Processing

End Uses: Ducts

Technical Data Sheet
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Knowde Enhanced TDS

Identification & Functionality

Polymer Name
Reinforcement Material
Composite Materials Functions

Features & Benefits

Materials Features
Key Features & Benefits

 

 

  • Provides a combination of high-strength and ablative properties for demanding applications
  • Low thermal expansion
  • Good Tack and Drape properties
  • Conforms to MIL-R-9299 Type B
Product Forms
  • Available on a wide variety of reinforcements, including fiberglass, graphite, and quartz
  • Also available as a Molding Compound and Bias Tape
  • Solution coated fabrics up to 152 cm wide
  • Compatible with Autoclave or Press Molding processes

Applications & Uses

Composites End Use
Composites Processing Methods
Applications / Qualifications
  • Rocket Nozzles
  • Ducting
  • Secondary Structure
Autoclave Cure Cycle
  • Apply 610 mmHg vacuum (minimum) for 1 hour before beginning heat cycle
  • Apply 689 KPa autoclave pressure
  • Raise product temperature from RT to 121°C at 1 - 3°C/min
  • Increase autoclave pressure to 276 KPa, vent vacuum at 103 – 138 KPa
  • Hold product at 121 ± 3°C for 30 minutes
  • Raise product temperature to 163 ± 3°C at 1 - 3°C/min
  • Hold product at cure temperature for 60 – 90 minutes
  • Cool to 66°C at no more than 5°C/min prior to releasing autoclave pressure
Optional Post Cure Cycle for High-Temp Applications
  • Heat Rise Rate between soak temperature: 1 – 5 °C/min
  • 121°C for 2 hours
  • 149°C for 1 hour
  • 177°C for 1 hour
  • 204°C for 1 hour
  • 218°C for 1 hour
  • 232°C for 2 hours
High Silica Phenolic Autoclave Cure Cycle
  • Apply 610 mmHg vacuum (minimum) for 1 hour before beginning heat cycle
  • Raise product temperature from RT to 93°C at 1 - 3°C/min
  • Apply autoclave pressure of 689 KPa, vent vacuum at 103 - 138 KPa
  • Raise product temperature to 177°C at 1 – 3°C /min
  • Hold product at 177 ± 3°C for 60 - 90 minutes
  • Cool to 66°C at 5°C/min prior to releasing autoclave pressure
  • Post Cure o Heat Oven to 177°C at 1 – 5°C /min and hold for 2 hours o Hold product at 204°C for 4 hours

Properties

Physical Properties
ValueUnitsTest Method / Conditions
Fabric Area Weight 617gsm
Prepreg Resin Content32 - 38%
Resin Flow (163°C, 103kPa)10 - 25%
Volatiles (135°C, 8 min)2 - 8%
Gel Time50-200Seconds
Mechanical Properties
ValueUnitsTest Method / Conditions
Hardness75BarcolASTM-D-2583
Per Ply Thickness0.016
Specific Gravity1.35g/ccASTM-D-792
Cure Cycle163°C Autoclave
Tensile Strength - Dry (24°C) 614MpaASTM-D-638
Tensile Modulus - Dry (24°C) 59.3GPaASTM-D-638
Compressive Strength - Dry (24°C) 531MPaASTM-D-695
Compressive Modulus - Dry (24°F) 64.1GPaASTM-D-695
Flexural Strength - Dry (24°C) 772MPaASTM-D-790
Flexural Modulus - Dry (24°C)55.8GPaASTM-D-790
Short Beam Shear - Dry (24°C)33.1MPaASTM-D-5379

Regulatory & Compliance

Quality Standards

Storage & Handling

Prepreg Storage Life
  • Out Life: 30 days @ 75°F
  • Shelf Life: 6 months @ 0°F and 3 months @ 40°F (dry)
  • **Store F-502 Silica at 0°F (dry)